Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
jet engine
|
| gptkbp:application |
military aircraft
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:designedBy |
gptkb:Tumansky_Design_Bureau
|
| gptkbp:diameter |
0.9 m
|
| gptkbp:engineConfiguration |
turbojet
|
| gptkbp:engineType |
axial compressor
single-stage turbine |
| gptkbp:firstFlight |
1955
|
| gptkbp:fuelType |
kerosene
annular combustion chamber |
| https://www.w3.org/2000/01/rdf-schema#label |
Tumansky R-25
|
| gptkbp:length |
3.5 m
|
| gptkbp:operationalArea |
1960s
|
| gptkbp:propulsion |
25 kN
|
| gptkbp:replacedBy |
gptkb:Tumansky_R-29
|
| gptkbp:successor |
gptkb:Tumansky_R-29
|
| gptkbp:type |
turbojet engine
|
| gptkbp:usedIn |
gptkb:Mikoyan-Gurevich_MiG-21
gptkb:Mikoyan_MiG-23 |
| gptkbp:weight |
400 kg
|